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You searched for subject:(Reentry vehicle). Showing records 1 – 6 of 6 total matches.

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Virginia Tech

1. Aubuchon, Vanessa V. Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics.

Degree: MS, Aerospace Engineering, 2013, Virginia Tech

 Currently, simulation predictions of the Orion Crew Module (CM) dynamics with drogue parachutes deployed are under-predicting the amount of damping as seen in free-flight tests.… (more)

Subjects/Keywords: parachutes; forced oscillation; damping; blunt body reentry vehicle; dynamic derivatives

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APA (6th Edition):

Aubuchon, V. V. (2013). Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics. (Masters Thesis). Virginia Tech. Retrieved from http://hdl.handle.net/10919/23327

Chicago Manual of Style (16th Edition):

Aubuchon, Vanessa V. “Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics.” 2013. Masters Thesis, Virginia Tech. Accessed April 15, 2021. http://hdl.handle.net/10919/23327.

MLA Handbook (7th Edition):

Aubuchon, Vanessa V. “Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics.” 2013. Web. 15 Apr 2021.

Vancouver:

Aubuchon VV. Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics. [Internet] [Masters thesis]. Virginia Tech; 2013. [cited 2021 Apr 15]. Available from: http://hdl.handle.net/10919/23327.

Council of Science Editors:

Aubuchon VV. Damping Effects of Drogue Parachutes on Orion Crew Module Dynamics. [Masters Thesis]. Virginia Tech; 2013. Available from: http://hdl.handle.net/10919/23327


Penn State University

2. Mirzaei, Mehrdad. OPTIMAL FEEDBACK CONTROL DESIGN FOR A HYPERSONIC REENTRY VEHICLE.

Degree: 2019, Penn State University

 The study of hypersonic flight is of utmost importance for commercial as well as military missions involving orbital and near orbital speeds. Hypersonic trajectory optimization… (more)

Subjects/Keywords: Optimal Control; Hamilton-Jacobi-Bellman Equation; Optimal Feedback Control; Trajectory Optimization; Hypersonic Reentry Vehicle; Sparse Collocation Method; Convex Optimization

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APA (6th Edition):

Mirzaei, M. (2019). OPTIMAL FEEDBACK CONTROL DESIGN FOR A HYPERSONIC REENTRY VEHICLE. (Thesis). Penn State University. Retrieved from https://submit-etda.libraries.psu.edu/catalog/17020mxm1533

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Mirzaei, Mehrdad. “OPTIMAL FEEDBACK CONTROL DESIGN FOR A HYPERSONIC REENTRY VEHICLE.” 2019. Thesis, Penn State University. Accessed April 15, 2021. https://submit-etda.libraries.psu.edu/catalog/17020mxm1533.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Mirzaei, Mehrdad. “OPTIMAL FEEDBACK CONTROL DESIGN FOR A HYPERSONIC REENTRY VEHICLE.” 2019. Web. 15 Apr 2021.

Vancouver:

Mirzaei M. OPTIMAL FEEDBACK CONTROL DESIGN FOR A HYPERSONIC REENTRY VEHICLE. [Internet] [Thesis]. Penn State University; 2019. [cited 2021 Apr 15]. Available from: https://submit-etda.libraries.psu.edu/catalog/17020mxm1533.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Mirzaei M. OPTIMAL FEEDBACK CONTROL DESIGN FOR A HYPERSONIC REENTRY VEHICLE. [Thesis]. Penn State University; 2019. Available from: https://submit-etda.libraries.psu.edu/catalog/17020mxm1533

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Tennessee – Knoxville

3. Davis, Chad Lee. A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2.

Degree: MS, Aerospace Engineering, 2011, University of Tennessee – Knoxville

  The space vehicle system concept (i.e. resupply vehicle) described is based on the new direction that President George W. Bush announced on January 14,… (more)

Subjects/Keywords: COTS; NASA; resupply vehicle; ISS; entry corridor; reentry analysis; Aerodynamics and Fluid Mechanics; Other Aerospace Engineering; Space Vehicles

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APA (6th Edition):

Davis, C. L. (2011). A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2. (Thesis). University of Tennessee – Knoxville. Retrieved from https://trace.tennessee.edu/utk_gradthes/965

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Davis, Chad Lee. “A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2.” 2011. Thesis, University of Tennessee – Knoxville. Accessed April 15, 2021. https://trace.tennessee.edu/utk_gradthes/965.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Davis, Chad Lee. “A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2.” 2011. Web. 15 Apr 2021.

Vancouver:

Davis CL. A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2. [Internet] [Thesis]. University of Tennessee – Knoxville; 2011. [cited 2021 Apr 15]. Available from: https://trace.tennessee.edu/utk_gradthes/965.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Davis CL. A Feasibility Study for Using Commercial Off The Shelf (COTS) Hardware for Meeting NASA’s Need for a Commercial Orbital Transportation Services (COTS) to the International Space Station - [COTS]2. [Thesis]. University of Tennessee – Knoxville; 2011. Available from: https://trace.tennessee.edu/utk_gradthes/965

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

4. Voelkel, Stephen Joseph. Thermal nonequilibrium models for high-temperature reactive processes.

Degree: PhD, Computational Science, Engineering, and Mathematics, 2016, University of Texas – Austin

 This dissertation examines how thermal nonequilibrium affects mixing and combustion in high-enthalpy, high-speed systems such as reentry vehicles, scramjets, and detonation-driven engines. Specifically, the focus… (more)

Subjects/Keywords: Thermal nonequilibrium; Scramjet; Reentry vehicle; Quasi-classical trajectory; QCT; Hydrogen combustion; Nitrogen dissociation; Nitrogen-oxygen scattering

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Voelkel, S. J. (2016). Thermal nonequilibrium models for high-temperature reactive processes. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/47234

Chicago Manual of Style (16th Edition):

Voelkel, Stephen Joseph. “Thermal nonequilibrium models for high-temperature reactive processes.” 2016. Doctoral Dissertation, University of Texas – Austin. Accessed April 15, 2021. http://hdl.handle.net/2152/47234.

MLA Handbook (7th Edition):

Voelkel, Stephen Joseph. “Thermal nonequilibrium models for high-temperature reactive processes.” 2016. Web. 15 Apr 2021.

Vancouver:

Voelkel SJ. Thermal nonequilibrium models for high-temperature reactive processes. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2016. [cited 2021 Apr 15]. Available from: http://hdl.handle.net/2152/47234.

Council of Science Editors:

Voelkel SJ. Thermal nonequilibrium models for high-temperature reactive processes. [Doctoral Dissertation]. University of Texas – Austin; 2016. Available from: http://hdl.handle.net/2152/47234


University of Maryland

5. Johnson, Joshua E. Aerothermodynamic Optimization of Earth Entry Blunt Body Heat Shields for Lunar and Mars Return.

Degree: Aerospace Engineering, 2009, University of Maryland

 A differential evolutionary algorithm has been executed to optimize the hypersonic aerodynamic and stagnation-point heat transfer performance of Earth entry heat shields for Lunar and… (more)

Subjects/Keywords: Engineering, Aerospace; aerothermodynamics; entry vehicle; heat shield; hypersonics; lunar and mars return; reentry

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Johnson, J. E. (2009). Aerothermodynamic Optimization of Earth Entry Blunt Body Heat Shields for Lunar and Mars Return. (Thesis). University of Maryland. Retrieved from http://hdl.handle.net/1903/9177

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Chicago Manual of Style (16th Edition):

Johnson, Joshua E. “Aerothermodynamic Optimization of Earth Entry Blunt Body Heat Shields for Lunar and Mars Return.” 2009. Thesis, University of Maryland. Accessed April 15, 2021. http://hdl.handle.net/1903/9177.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

MLA Handbook (7th Edition):

Johnson, Joshua E. “Aerothermodynamic Optimization of Earth Entry Blunt Body Heat Shields for Lunar and Mars Return.” 2009. Web. 15 Apr 2021.

Vancouver:

Johnson JE. Aerothermodynamic Optimization of Earth Entry Blunt Body Heat Shields for Lunar and Mars Return. [Internet] [Thesis]. University of Maryland; 2009. [cited 2021 Apr 15]. Available from: http://hdl.handle.net/1903/9177.

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation

Council of Science Editors:

Johnson JE. Aerothermodynamic Optimization of Earth Entry Blunt Body Heat Shields for Lunar and Mars Return. [Thesis]. University of Maryland; 2009. Available from: http://hdl.handle.net/1903/9177

Note: this citation may be lacking information needed for this citation format:
Not specified: Masters Thesis or Doctoral Dissertation


University of Texas – Austin

6. Ulerich, Rhys David. Reducing turbulence- and transition-driven uncertainty in aerothermodynamic heating predictions for blunt-bodied reentry vehicles.

Degree: PhD, Computational Science, Engineering, and Mathematics, 2014, University of Texas – Austin

 Turbulent boundary layers approximating those found on the NASA Orion Multi-Purpose Crew Vehicle (MPCV) thermal protection system during atmospheric reentry from the International Space Station… (more)

Subjects/Keywords: Atmospheric reentry; B-spline collocation; Channel flow; Cold wall; Direct numerical simulation; Energy perturbation method; Favorable pressure gradient; Flat plate; Homogenized boundary layer; Inviscid base flow; Isothermal wall; Low Reynolds number; Manufactured solution; NASA Orion; Negative displacement thickness; Predictive computation; Pseudospectral method; Radial nozzle; Reducing uncertainty; Reentry vehicle; Relaminarization; Sampling uncertainty; Simulation framework; Slow growth formulation; Software verification; Transition modeling; Turbulence budgets; Turbulent boundary layer; Wall blowing; Wall transpiration

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APA · Chicago · MLA · Vancouver · CSE | Export to Zotero / EndNote / Reference Manager

APA (6th Edition):

Ulerich, R. D. (2014). Reducing turbulence- and transition-driven uncertainty in aerothermodynamic heating predictions for blunt-bodied reentry vehicles. (Doctoral Dissertation). University of Texas – Austin. Retrieved from http://hdl.handle.net/2152/26886

Chicago Manual of Style (16th Edition):

Ulerich, Rhys David. “Reducing turbulence- and transition-driven uncertainty in aerothermodynamic heating predictions for blunt-bodied reentry vehicles.” 2014. Doctoral Dissertation, University of Texas – Austin. Accessed April 15, 2021. http://hdl.handle.net/2152/26886.

MLA Handbook (7th Edition):

Ulerich, Rhys David. “Reducing turbulence- and transition-driven uncertainty in aerothermodynamic heating predictions for blunt-bodied reentry vehicles.” 2014. Web. 15 Apr 2021.

Vancouver:

Ulerich RD. Reducing turbulence- and transition-driven uncertainty in aerothermodynamic heating predictions for blunt-bodied reentry vehicles. [Internet] [Doctoral dissertation]. University of Texas – Austin; 2014. [cited 2021 Apr 15]. Available from: http://hdl.handle.net/2152/26886.

Council of Science Editors:

Ulerich RD. Reducing turbulence- and transition-driven uncertainty in aerothermodynamic heating predictions for blunt-bodied reentry vehicles. [Doctoral Dissertation]. University of Texas – Austin; 2014. Available from: http://hdl.handle.net/2152/26886

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